| 制导刚度受限时不同结构驾驶仪对制导精度的影响分析 |
| |
| 引用本文： | 栗金平,黎海青,张晓峰,张正同. 制导刚度受限时不同结构驾驶仪对制导精度的影响分析[J]. 弹箭与制导学报, 2017, 37(1). DOI: 10.15892/j.cnki.djzdxb.2017.01.001 |
| |
| 作者姓名： | 栗金平 黎海青 张晓峰 张正同 |
| |
| 作者单位： | 中国兵器工业第203研究所,西安,710065 |
| |
| 摘 要： | 为有效提高比例导引制导反坦克导弹近射程作战能力,需研究制导刚度受限时,不同结构自动驾驶仪对制导精度的影响.首先对反坦克导弹比例导引制导系统形式进行了阐述;然后给出常用的自动驾驶仪,并对不同自动驾驶仪的动态性能进行对比分析;最后分析对应的线性比例导引制导系统模型,得出在制导刚度受限条件下,阻尼回路自动驾驶仪对应制导系统制导精度最高.
|
| 关 键 词： | 比例导引 自动驾驶仪 频域分析 时域分析 |
The Impact Analysis of Autopilots with Different Structures on Guidance Accuracy when the Guidance Stiffness was Constrained |
| |
| LI Jinping,LI Haiqing,ZHANG Xiaofeng,ZHANG Zhengtong. The Impact Analysis of Autopilots with Different Structures on Guidance Accuracy when the Guidance Stiffness was Constrained[J]. Journal of Projectiles Rockets Missiles and Guidance, 2017, 37(1). DOI: 10.15892/j.cnki.djzdxb.2017.01.001 |
| |
| Authors: | LI Jinping LI Haiqing ZHANG Xiaofeng ZHANG Zhengtong |
| |
| Abstract: | In order to improve the combat capability of the anti tank missile using the proportional navigation in the near range,the influence of the autopilots with different structures on the guidance accuracy was studied.First,the form of the anti tank missile's guidance system using the proportional navigation was described.Then,the common autopilot was given,and the dynamic performance of different autopilots was compared and analyzed.At last,the corresponding linear proportional navigation guidance system model was analyzed.It was concluded that the guidance precision of corresponding guidance system of damping loop autopilot was the highest under the condition of limited guidance stiffness. |
| |
| Keywords: | proportional navigation autopilot frequency domain analysis time domain analysis |
| 本文献已被 万方数据 等数据库收录！ |
|
